BRPI0614795A8 - Disposição de aleta diretriz de uma turbomáquina - Google Patents

Disposição de aleta diretriz de uma turbomáquina

Info

Publication number
BRPI0614795A8
BRPI0614795A8 BRPI0614795A BRPI0614795A BRPI0614795A8 BR PI0614795 A8 BRPI0614795 A8 BR PI0614795A8 BR PI0614795 A BRPI0614795 A BR PI0614795A BR PI0614795 A BRPI0614795 A BR PI0614795A BR PI0614795 A8 BRPI0614795 A8 BR PI0614795A8
Authority
BR
Brazil
Prior art keywords
guide vane
arrangement
carrying portion
turbomachine
guideline
Prior art date
Application number
BRPI0614795A
Other languages
English (en)
Portuguese (pt)
Inventor
Chekanov Alexander
Khanin Alexander
Original Assignee
Alstom Technology Ltd
General Electric Technology Gmbh
Ansaldo Energia Switzerland AG
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Alstom Technology Ltd, General Electric Technology Gmbh, Ansaldo Energia Switzerland AG filed Critical Alstom Technology Ltd
Publication of BRPI0614795A2 publication Critical patent/BRPI0614795A2/pt
Publication of BRPI0614795A8 publication Critical patent/BRPI0614795A8/pt

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/042Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246Fastening of diaphragms or stator-rings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Vessels And Coating Films For Discharge Lamps (AREA)
  • Rotary Pumps (AREA)
  • Motor Or Generator Frames (AREA)
  • Control Of Turbines (AREA)
BRPI0614795A 2005-08-17 2006-08-09 Disposição de aleta diretriz de uma turbomáquina BRPI0614795A8 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
CH1348/05 2005-08-17
CH13482005 2005-08-17
PCT/EP2006/065188 WO2007020217A2 (fr) 2005-08-17 2006-08-09 Dispositif d'aube directrice d'une turbomachine

Publications (2)

Publication Number Publication Date
BRPI0614795A2 BRPI0614795A2 (pt) 2011-04-12
BRPI0614795A8 true BRPI0614795A8 (pt) 2017-07-25

Family

ID=34975062

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0614795A BRPI0614795A8 (pt) 2005-08-17 2006-08-09 Disposição de aleta diretriz de uma turbomáquina

Country Status (10)

Country Link
US (1) US7677867B2 (fr)
EP (1) EP1917419B1 (fr)
AT (1) ATE430874T1 (fr)
BR (1) BRPI0614795A8 (fr)
CA (1) CA2617826C (fr)
DE (1) DE502006003679D1 (fr)
MX (1) MX2008002013A (fr)
SI (1) SI1917419T1 (fr)
TW (1) TWI324217B (fr)
WO (1) WO2007020217A2 (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102007015669A1 (de) * 2007-03-31 2008-10-02 Mtu Aero Engines Gmbh Turbomaschine
US9133732B2 (en) 2010-05-27 2015-09-15 Siemens Energy, Inc. Anti-rotation pin retention system
US20120321454A1 (en) * 2011-06-14 2012-12-20 Yu Zhi-Xuan Wind power generation apparatus
US10526921B2 (en) * 2017-06-15 2020-01-07 General Electric Company Anti-rotation shroud dampening pin and turbine shroud assembly
US11346252B2 (en) 2019-07-01 2022-05-31 Raytheon Technologies Corporation Multi-purpose anti-rotation lock pin
CN113605994B (zh) * 2021-07-26 2023-10-03 中国船舶重工集团公司第七0三研究所 一种新型船用燃气轮机低泄露损失双联冷却导叶结构

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB804922A (en) * 1956-01-13 1958-11-26 Rolls Royce Improvements in or relating to axial-flow fluid machines for example compressors andturbines
GB804010A (en) * 1956-02-13 1958-11-05 Rolls Royce Improvements in or relating to stator vane assemblies such as are used in axial-flowfluid machines
GB995643A (en) * 1961-12-27 1965-06-23 Licentia Gmbh Improvements in or relating to multistage steam turbines and installations thereof
US3471126A (en) * 1966-10-31 1969-10-07 United Aircraft Corp Movable vane unit
JPS5872606A (ja) 1981-10-24 1983-04-30 Hitachi Zosen Corp ピストン制御孔型排気制御装置
US5022818A (en) * 1989-02-21 1991-06-11 Westinghouse Electric Corp. Compressor diaphragm assembly
US5131814A (en) * 1990-04-03 1992-07-21 General Electric Company Turbine blade inner end attachment structure
US5498126A (en) * 1994-04-28 1996-03-12 United Technologies Corporation Airfoil with dual source cooling
EP0943785A1 (fr) * 1998-03-18 1999-09-22 Asea Brown Boveri AG Fixation d'une aube à un stator
JP2000213301A (ja) 1999-01-19 2000-08-02 Takeshi Hatanaka 高効率タ―ビン
JP2002201913A (ja) * 2001-01-09 2002-07-19 Mitsubishi Heavy Ind Ltd ガスタービンの分割壁およびシュラウド
DE10210866C5 (de) * 2002-03-12 2008-04-10 Mtu Aero Engines Gmbh Leitschaufelbefestigung in einem Strömungskanal einer Fluggasturbine
GB0228748D0 (en) * 2002-12-10 2003-01-15 Alstom Switzerland Ltd Sealing arrangement
US7014424B2 (en) 2003-04-08 2006-03-21 United Technologies Corporation Turbine element
US6832897B2 (en) 2003-05-07 2004-12-21 General Electric Company Second stage turbine bucket airfoil
US7094025B2 (en) * 2003-11-20 2006-08-22 General Electric Company Apparatus and methods for removing and installing a selected nozzle segment of a gas turbine in an axial direction
US7094026B2 (en) * 2004-04-29 2006-08-22 General Electric Company System for sealing an inner retainer segment and support ring in a gas turbine and methods therefor

Also Published As

Publication number Publication date
MX2008002013A (es) 2008-03-27
CA2617826A1 (fr) 2007-02-22
TWI324217B (en) 2010-05-01
WO2007020217A2 (fr) 2007-02-22
EP1917419A2 (fr) 2008-05-07
SI1917419T1 (sl) 2009-10-31
US7677867B2 (en) 2010-03-16
WO2007020217A3 (fr) 2007-04-12
ATE430874T1 (de) 2009-05-15
CA2617826C (fr) 2014-04-01
TW200712309A (en) 2007-04-01
US20080199312A1 (en) 2008-08-21
DE502006003679D1 (de) 2009-06-18
BRPI0614795A2 (pt) 2011-04-12
EP1917419B1 (fr) 2009-05-06

Similar Documents

Publication Publication Date Title
DE602006002673D1 (de) Vibrationsdämpfungselemente für einen axialen Haltering von Bläserschaufeln einer Turbomaschine
BRPI0614795A8 (pt) Disposição de aleta diretriz de uma turbomáquina
EP2204539A3 (fr) Ensemble de stator pour un moteur de turbine à gaz
SE0700823L (sv) Komponent för en gasturbinmotor, jetmotor försedd med en sådan komponent, samt en flygmaskin försedd med en sådan jetmotor
GB2467897A (en) Turbine nozzle segment and assembly
DE502005006133D1 (de) Gasturbine, insbesondere flugtriebwerk
DE60125441D1 (de) Mehrstufiges, mehrebenes Vebrennungssystem für Gasturbine
GB0903050D0 (en) Shroud-Diffuser assembly
ATE522702T1 (de) Variable düse für einen turbolader mit durch radiale glieder positioniertem düsenring
DE502004006868D1 (de) Gasturbine, insbesondere flugtriebwerk
RU2005129351A (ru) Турбинный модуль для газотурбинного двигателя
DE502005007638D1 (de) Lamellendichtung, insbesondere für eine gasturbine
ATE521812T1 (de) Gehäuse für ein sich bewegendes laufrad einer turbomaschine
SE0300770L (sv) Förfarande för framställning av en statorkomponent
ATE486223T1 (de) Lüfterrad
DE502004011910D1 (de) Stationäre gasturbine
EP1586741A3 (fr) Dispositif pour amortir les vibrations des aubes de guidage d'une turbine à gaz
ATE539235T1 (de) Konfiguration von aufnahmenuten für turbinenschaufeln
BRPI0912030B8 (pt) união de elementos de rotor ou de estator de uma turbomáquina e turbomáquina, tal como um turborreator ou um turbopropulsor
JP2012031865A5 (fr)
BRPI0907645A2 (pt) Difusor para uma turbomáquina e turbomáquina, como um turborreator ou um turbopropulsor de avião
RU2013108685A (ru) Турбинная система (варианты)
ATE538300T1 (de) System zum mischen von gasströmen in einem gasturbinentriebwerk, zugehöriges gasturbinentriebwerk und flugzeugtriebwerk
WO2011153393A3 (fr) Structure d'étanchéité de turbine à gaz
ATE455935T1 (de) Leitvorrichtung einer strömungsmaschine sowie leitschaufel für eine derartige leitvorrichtung

Legal Events

Date Code Title Description
B25D Requested change of name of applicant approved

Owner name: ALSTOM TECHNOLOGY LTD. (CH) , GENERAL ELECTRIC TEC

B25A Requested transfer of rights approved

Owner name: ANSALDO ENERGIA SWITZERLAND AG (CH)

B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]
B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2474 DE 05-06-2018 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.